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In the Spring 2004 Issue of
The Rolls-Royce Eagle 22
While it is a near certainty that few will ever see inside a real Eagle 22, images of Barry Hares' model, in conjunction with his account of its gestation, provide a unique opportunity to better understand a truly spectacular aircraft engine.
V-3420-B10 Timing
Performance guarantees had been based on testing using an engine configured as a V-3420A to enable its running on the available Allison altitude test stand. So configured, the test engine used the standard V-3420A firing order with each of the 24 cylinders firing 30 degrees apart. As designed and delivered the B-10 engine used 60 degree firing, i.e. simultaneous firing of two cylinders (one in each vee), referred to as “zero” phasing by Allison. When the engines were run in the altitude dynamometer it was found that the B-10 was about 3 percent low on power. In an effort to restore this power Allison adopted an alternate firing scheme known as 150 degree phasing and utilized a 30 degree interval. Historically, the details of how they accomplished this have been a mystery. Allison Competition Engines recently had an opportunity to teardown a B-10 known to have been modified with the 150 degree phasing. By taking careful notes of the as-found configuration we are now able to provide the details.
The WW II Engines of Packard
If we immediately cut to the basics, we can say that the only similarities are the fact that they are both 60º V-12 water-cooled engines. Neither is an evolution of the design of the other. Their only connection is the fact that both were built by Packard during World War II. This article briefly traces the origins of each and describe its design.
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